View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 32785U 08021C 23090.13151269 .00008518 00000-0 85299-3 0 9996
2 32785 97.6982 57.8323 0012706 12.8115 347.3424 14.91574904809255
| Epoch (UTC): | 31 March 2023 03:09:22 |
| Eccentricity: | 0.0012706 |
| inclination: | 97.6982° |
| perigee height: | 584 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 57.8323° |
| argument of perigee: | 12.8115° |
| revolutions per day: | 14.91574904 |
| mean anomaly at epoch: | 347.3424° |
| orbit number at epoch: | 80925 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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